US4149689A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Protective screen for jet-engine intake
Assignee: Individual
•
Filing: 1977-07-01
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Granted: 1979-04-17
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Expires: 1997-07-01
Abstract
Abstract The forwardly open intake end of a jet engine, powering an aircraft, is screened against birds and other airborne objects by a conical cage formed from an array of metal rods converging on the engine axis, the rods being held together at the vertex of the cone by a solid tip and in an intermediate plane as well as at the cone base by a pair of metal rings. In flight, they are free to vibrate so as to shake off adhering ice particles. De-icing can be further promoted by feeding back exhaust gases from the rear of the engine to the interior of the cage through an external pipe.
Inventors
- 👤 John McDonald
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 17:47
CPC Classifications
B; B64; B64D; B64D33/00; B64D33/02; F; F02; F02C; F02C7/00; F02C7/04; F02C7/05; F02C7/055; B64D2033/022
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
144 words
In an aircraft having a jet engine mounted in a forwardly and rearwardly open nacelle with an axis oriented in the direction of flight, said jet engine having an air intake at the front end of said nacelle, the combination therewith of a protective screen for said air intake, said screen being essentially constituted by a frustoconical array of a multiplicity of closely spaced straight resilient metal rods surrounding the front end of said nacelle and converging forwardly therefrom, a pointed tip substantially in line with said axis for holding the forward ends of said rods together, said rods being mutually unconnected over a substantial part of their length to facilitate their vibration in flight, certain of said rods being foreshortened to provide an access opening in the vicinity of said front end, and door means on said screen normally closing said access opening.
Claim 2
Dependent Claim
144 words
In an aircraft having a jet engine mounted in a forwardly and rearwardly open nacelle with an axis oriented in the direction of flight, said jet engine having an air intake at the front end of said nacelle, the combination therewith of a protective screen for said air intake, said screen being essentially constituted by a frustoconical array of a multiplicity of closely spaced straight resilient metal rods surrounding the front end of said nacelle and converging forwardly therefrom, a pointed tip substantially in line with said axis for holding the forward ends of said rods together, said rods being mutually unconnected over a substantial part of their length to facilitate their vibration in flight, certain of said rods being foreshortened to provide an access opening in the vicinity of said front end, and door means on said screen normally closing said access opening.
Claim 3
Dependent Claim
24 words
The combination defined in claim 1 wherein said door means comprises a cover axially slidable along a pair of rails adjoining said access opening.
Claim 4
Dependent Claim
33 words
The combination defined in claim 1, further comprising conduit means extending from the rear end of said nacelle to the interior of said screen for feeding back exhaust gases to de-ice said rods.
Claim 5
Dependent Claim
46 words
The combination defined in claim 3 wherein said tip is hollow, said conduit means comprising a pipe on the outside of said nacelle terminating at said hollow tip and deflector means in said tip for directing said exhaust gases against inner surface portions of said rods.
Claim 6
Dependent Claim
46 words
The combination defined in claim 1 wherein said screen is provided with a retaining ring lying in a plane transverse to said axis and interconnecting said rods at a location generally midway of their length, said rods being mutually unconnected between said ring and said tip.
Claim 7
Dependent Claim
47 words
The combination defined in claim 5 wherein said screen is further provided with a mounting ring connected with said rods and secured to said nacelle, said rods being mutually unconnected between said rings with freedom to vibrate between said tip, said retaining ring and said mounting ring.
Claim 8
Dependent Claim
19 words
The combination defined in claim 1 wherein said rods include with said axis an angle not exceeding about 30°.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-04-16 | 1982-10-16 | 1983-04-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-04-16 | 1986-10-16 | 1987-04-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-04-16 | 1990-10-16 | 1991-04-17 | $7700.00 | Window Closed / Lapsed |